Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the RWD-14b Army Cooperation Aircraft.
1 x PZL G-1620B Mors-II 9-cylinder, air-cooled radial piston engine developing 470 horsepower driving two-bladed propeller unit at the nose.
Propulsion
155 mph
250 kph | 135 kts
Max Speed
16,732 ft
5,100 m | 3 miles
Service Ceiling
419 miles
675 km | 364 nm
Operational Range
1,200 ft/min
366 m/min
Rate-of-Climb